The relationship between the electrical conductivity and temperature of Canadian produced wide-cut and kerosine type aviation turbine fuels containing static dissipator additives has been evaluated. Results obtained show that the temperature/conductivity coefficient, n, in the relationship log kt = n (t - t1) log kt1 is dependent upon several factors including (a) temperature range (b) fuel type (c) additive type. lt is recommended that the results of the evaluation be summarized and presented in the form of a test procedure which can be reference in aviation fuel specifications.